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CFD Method for Aircraft Skid Performance Including Wear and Heat Transfer
Technical Paper
2008-01-2249
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
A CFD method for predicting wear and heat transfer for an aircraft skid is described. It uses a finite volume method with a moving grid to account for wear. Therefore the skid material flows through the grid. The interface between the skid and runway is modeled empirically and is based on test data. A calculation for a simple skid is presented. The code is written in Mathematica which runs quickly and therefore is useful for experimenting with physical models and conducting trade studies.
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Citation
Carroll, G., "CFD Method for Aircraft Skid Performance Including Wear and Heat Transfer," SAE Technical Paper 2008-01-2249, 2008, https://doi.org/10.4271/2008-01-2249.Also In
References
- Metallic Materials Properties Development and Standardization 03. Federal Aviation Administration 2006
- Kreith F Goswami Y. CRC Handbook of Mechanical Engineering. 2 nd edn 3 130 CRC Press 2004
- Navaratnam K. Dong-dae Lee Parameswaran S. “Application of a Novel Moving-Grid Methodology to Model the Interaction of a Synthetic Jet with a Turbulent Boundary Layer” Numerical Heat Transfer: Part B: Fundamentals 49 2006 105 123